ATBECHDEDKESFRGBGRITLILUNLSEMCPTIESILTLVFIROMKCY..TRBGCZEEHUPLSK..HRIS..MTNO....SM..................JJDIM360 Ver 1.28 (29 Oct 2014) - 1620000/02157306EUROPEAN PATENT APPLICATIONA320170118EP09168405.020090821enenen19589920080821US2017011820170320100224201008F02K 7/02 20060101AFI20161215BHEP F02K 1/00 20060101ALI20161215BHEP F02K 1/28 20060101ALI20161215BHEP F02K 7/075 20060101ALI20161215BHEP F02C 5/02 20060101ALI20161215BHEP F23R 7/00 20060101ALI20161215BHEP dePulsierendes Detonations- Verpuffungssystem und Verfahren zur Erleichterung der Produktion von Detonations zu Verpuffungs WellenenPulse detonation/deflagration apparatus and method for enhancing the production of detonation to deflagration wavesfrSystème de détonation/déflagration pulsée et procédé pour améliorer la production d'ondes de détonation en déflagration1Lockheed Martin Corporation (Maryland Corp.)100983697FB22082/G12440E6801 Rockledge DriveBethesda MD 20817USBoespflug, Matthew Patrick307 Moe RoadClifton Park, NY 12065USSteenburgh, DennisPO Box 293Caroga Lake, NY 12032USSaddoughi, Seyed Gholami639 Bruno RoadClifton Park, NY 12065USBennett, Grover Andrew1036 Wavell RoadSchenectady, NY 12303USSessford, Russellet al101298678Forresters Skygarden Erika-Mann-Strasse 1180636 MünchenDEATBEBGCHCYCZDEDKEEESFIFRGBGRHRHUIEISITLILTLULVMCMKMTNLNOPLPTROSESISKSMTR20170118201703

Pulse detonation/deflagration apparatus (30, 30') for providing enhanced pressure wave operating frequency and/or magnitude, and methods of increasing the frequency or the magnitude of deflagration to detonation waves (37), are provided. A pulse detonation/deflagration apparatus (30, 30') can include a main/outer pulse detonation/deflgration actuator/engine (31) with multiple smaller internal combustion chambers or tubes (33) positioned inside the cavity of the main/outer actuator/engine (31) with each performing the function of individual pulse detonation/deflagration actuator/engines (31), The output pressure waves (37) created by the internal combustion chambers or tubes (33) can be utilized for propulsion or for controlling large scale flows, where needed.

FB22082/G12440EEP09168405.0Lockheed Martin Corporation (Maryland Corp.)1DH20161221F02KF02CF23RF23CUS2705396ABOYCE ARTHUR L ET AL19550405X1,3-10,12-16* column 1, line 19 - line 29 ** column 2, line 52 - column 3, line 43 ** column 4, line 1 - line 29 ** column 4, line 84 - column 5, line 52 ** column 6, line 21 - line 31 ** figures *US2888803ALEMUEL PON19590602X1-3,5-8,11,13,15-17* column 2, line 19 - line 56 ** column 3, line 43 - line 50 ** column 4, line 54 - column 5, line 20 ** figures *US6003301ABRATKOVICH THOMAS E [US] ET AL19991221X1-4,6,7,11,13,15,17* column 1, line 43 - column 2, line 20 ** column 4, line 66 - column 6, line 53 ** column 8, line 35 - line 40 ** figures 1-13 *US6439503B1WINFREE DON D [US] ET AL20020827X1,4,6,7,11,13,15* column 1, line 11 - line 20 ** column 2, line 43 - column 3, line 54 ** column 4, line 22 - column 5, line 4 ** column 5, line 50 - line 67 ** abstract; figures *US2008087010A1EDELMAN RAYMOND B [US] ET AL20080417X1,2,6-8,11-13,15-17* paragraph [0017] - paragraph [0020] ** abstract; figure 1 *O'Shea, GearóidThe Hague20161214US2705396A19550405NONEUS2888803A19590602NONEUS6003301A19991221NONEUS6439503B120020827NONEUS2008087010A120080417NONE